Influence of rotor–stator component partition structure on the aerodynamic performance of centrifugal compressors-Reference-Cited by-同舟云学术

Influence of rotor–stator component partition structure on the aerodynamic performance of centrifugal compressors

Published:2019-01-01 Issue:1 Volume:13 Page:1080-1094
ISSN:1994-2060
Container-title:Engineering Applications of Computational Fluid Mechanics
language:en
Short-container-title:Engineering Applications of Computational Fluid Mechanics

Author:

Li Chunyang¹^ORCID,Ji Chunjun¹²,Shi Mao³,Sun Qi⁴

Affiliation:

1. School of Energy and Power Engineering, Dalian University of Technology, Dalian, People’s Republic of China

2. Key Laboratory of Ocean Energy Utilization and Energy Conservation of Ministry of Education, Dalian University of Technology, Dalian, People’s Republic of China

3. Dalian Zhongyi Turbin Technology Co., Ltd., Dalian, People’s Republic of China

4. Institute of Engineering Thermophysics, Chinese Academy of Sciences, Beijing, People’s Republic of China

Publisher

Informa UK Limited

Subject

Modeling and Simulation,General Computer Science

Link

https://www.tandfonline.com/doi/pdf/10.1080/19942060.2019.1669075

Reference36 articles.

1. Annular Cascade for Radial Compressor Development

2. Experimental and computational fluid dynamics-based numerical simulation of using natural gas in a dual-fueled diesel engine

3. Computational investigation of impeller—diffuser interaction in a centrifugal compressor with different types of diffusers

4. Numerical investigation of the effect of leakage flow through erosion-induced clearance gaps of guide vanes on the performance of Francis turbines

5. Numerical simulation of nanofluid flow inside a root canal

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